Spacecraft attitude control with simultaneous unloading of the angular momentum of inertial actuators
| Autor: | V. N. Ryabchenko, N. E. Zubov, E. A. Mikrin, M. Sh. Misrikhanov |
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| Rok vydání: | 2015 |
| Předmět: |
Physics
Angular momentum Inertial frame of reference Computer Networks and Communications business.industry Applied Mathematics Robotics Theoretical Computer Science Control and Systems Engineering Control theory Computer Vision and Pattern Recognition Circular orbit Artificial intelligence Multiplicity (chemistry) Algebraic number Actuator business Software Eigenvalues and eigenvectors Information Systems |
| Zdroj: | Journal of Computer and Systems Sciences International. 54:621-628 |
| ISSN: | 1555-6530 1064-2307 |
| Popis: | A method is proposed for solving the problem of controlling finite eigenvalues of a descriptor linear dynamic system, which is based on the original decomposition of the model of the initial system that is unsolved for the derivatives and is defined in the space of states. This method has no restrictions on the algebraic and geometric multiplicity of the finite eigenvalues and enables analytical synthesis of control laws. Using the proposed method in the case of circular orbits, we obtain the analytical solution for the problem of spacecraft attitude control with simultaneous unloading of the angular momentum of the inertial actuators. The results of the mathematical modeling are presented. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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